Airworthiness Directives; Agusta S.p.A. Model A109A and A109A II Helicopters
airworthiness · Rule · Final rule. · Published 2008-11-25 · Effective 2008-12-30 · 73 FR 71526
Document
Document number
E8-27611
Federal Register citation
73 FR 71526
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Agusta S.p.A. Model A109A and A109A II
Publication date
2008-11-25
Effective date
2008-12-30
FAA docket
Docket No. FAA-2008-0834
Abstract
This amendment supersedes an existing airworthiness directive (AD) for the specified Agusta S.p.A. (Agusta) model helicopters. This AD results from a revised mandatory continuing airworthiness information (MCAI) issued by an aviation authority to identify and correct an unsafe condition on an aviation product. The aviation authority of Italy, with which we have a bilateral agreement, reports that the previous MCAI should not apply to newly redesigned and improved tail rotor blades. This AD requires the same inspections as the current AD but limits the applicability to only three part-numbered tail rotor blades. This AD requires actions that are intended to prevent fatigue failure of a tail rotor blade (blade), loss of a tail rotor, and subsequent loss of control of the helicopter.